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A thrust ring for an undercarriage in a track-type machine includes an annular body having an outer circular edge and an inner circular edge defining a common center axis. A first set of oil grooves and a first set of thrust faces are positioned in an alternating arrangement on each of a first axial

A thrust ring for an undercarriage in a track-type machine includes an annular body having an outer circular edge and an inner circular edge defining a common center axis. A first set of oil grooves and a first set of thrust faces are positioned in an alternating arrangement on each of a first axial side and a second axial side of the annular body. Each of the oil grooves includes a cross sectional contour shaped to balance an oil flow property of the thrust ring with a strength property of the thrust ring, and defining a non-uniform curve which includes a plurality of curve segments each having a different radial attribute. The thrust ring defines a Plouzek value equal to 1.

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1. A thrust ring for an undercarriage in a track-type machine comprising: an annular body including an outer circular edge and an inner circular edge defining a common center axis, the annular body further including a first thrust surface on a first axial side of the annular body and a second thrust

1. A thrust ring for an undercarriage in a track-type machine comprising: an annular body including an outer circular edge and an inner circular edge defining a common center axis, the annular body further including a first thrust surface on a first axial side of the annular body and a second thrust surface on a second axial side of the annular body;the first thrust surface having a first set of oil grooves formed therein at spaced apart locations about the center axis, and a first set of thrust faces positioned in an alternating arrangement with the first set of oil grooves; andthe second thrust surface having a second set of oil grooves formed therein and positioned at spaced apart locations about the center axis which are offset from locations of the first set of oil grooves, and a second set of thrust faces positioned in an alternating arrangement with the second set of oil grooves;wherein each of the oil grooves extends from the inner circular edge to the outer circular edge and defines a throat area for supplying lubricating oil to the thrust faces on the corresponding axial side of the annular body, and each of the thrust faces extends from the inner circular edge to the outer circular edge and defines a face loading area for reacting face loads through the thrust ring; andwherein each of the oil grooves further includes a first lip surface and a second lip surface adjoining a first adjacent thrust face and a second adjacent thrust face, respectively, each of the first lip surface and the second lip surface defining a convex radius of curvature; a first transition surface and a second transition surface adjoining the first lip surface and the second lip surface, respectively, each of the first transition surface and the second transition surface defining a first concave radius of curvature which is less than the convex radius of curvature; and a basal surface adjoining each of the first transition surface and the second transition surface, the basal surface defining a second concave radius of curvature which is greater than the first concave radius of curvature and greater than the convex radius of curvature. 2. The thrust ring of claim 1 wherein each of the oil grooves includes a uniform longitudinal contour extending from the inner circular edge to the outer circular edge, the uniform longitudinal contour lying in a first plane which includes a plane of the center axis, and wherein each of the oil grooves further includes a non-uniform cross sectional contour extending from the first adjacent thrust face to the second adjacent thrust face, the non-uniform cross sectional contour lying in a second plane which is normal to the first plane and parallel the center axis. 3. The thrust ring of claim 1 wherein the first concave radius of curvature is equal to about 0.15 millimeters, and wherein the second concave radius of curvature is equal to about 0.25 millimeters. 4. The thrust ring of claim 1 wherein the second concave radius of curvature defines a circle, the circle including a plurality of surface points of each of the first transition surface and the second transition surface, and a plurality of surface points of each of the first lip surface and the second lip surface. 5. The thrust ring of claim 1 wherein each of the first set of oil grooves and the second set of oil grooves includes a total of two oil grooves, and wherein each of the first set of thrust faces and the second set of thrust faces includes a total of two thrust faces. 6. The thrust ring of claim 5 wherein the oil grooves of the first set are positioned about 180° from one another about the center axis, and wherein the oil grooves of the second set are positioned about 180° from one another about the center axis, and wherein each of the oil grooves of the first set are positioned about 90° from the oil grooves of the second set about the center axis.